GB2249510A - Tapping threaded holes - Google Patents
Tapping threaded holes Download PDFInfo
- Publication number
- GB2249510A GB2249510A GB9119619A GB9119619A GB2249510A GB 2249510 A GB2249510 A GB 2249510A GB 9119619 A GB9119619 A GB 9119619A GB 9119619 A GB9119619 A GB 9119619A GB 2249510 A GB2249510 A GB 2249510A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tool
- component
- fluid
- hole
- rings
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000010079 rubber tapping Methods 0.000 title description 2
- 239000012530 fluid Substances 0.000 claims abstract description 27
- 239000000463 material Substances 0.000 claims abstract description 20
- 229910052751 metal Inorganic materials 0.000 claims abstract description 9
- 239000002184 metal Substances 0.000 claims abstract description 9
- 239000011156 metal matrix composite Substances 0.000 claims abstract description 9
- 239000011159 matrix material Substances 0.000 claims abstract description 3
- 238000000034 method Methods 0.000 claims description 20
- 239000000314 lubricant Substances 0.000 claims description 11
- 239000002245 particle Substances 0.000 claims description 10
- 229910000831 Steel Inorganic materials 0.000 claims description 7
- 239000004411 aluminium Substances 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 239000010959 steel Substances 0.000 claims description 7
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 5
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 5
- 239000003921 oil Substances 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 2
- 239000010941 cobalt Substances 0.000 claims description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 2
- 239000011819 refractory material Substances 0.000 claims 2
- 229910001315 Tool steel Inorganic materials 0.000 claims 1
- HMDDXIMCDZRSNE-UHFFFAOYSA-N [C].[Si] Chemical compound [C].[Si] HMDDXIMCDZRSNE-UHFFFAOYSA-N 0.000 claims 1
- 238000009760 electrical discharge machining Methods 0.000 claims 1
- 238000004663 powder metallurgy Methods 0.000 claims 1
- 239000007788 liquid Substances 0.000 description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 3
- 239000011777 magnesium Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910000861 Mg alloy Inorganic materials 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910052580 B4C Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000010408 film Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23G—THREAD CUTTING; WORKING OF SCREWS, BOLT HEADS, OR NUTS, IN CONJUNCTION THEREWITH
- B23G5/00—Thread-cutting tools; Die-heads
- B23G5/005—Thread-cutting tools; Die-heads with lubrication or cooling devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23G—THREAD CUTTING; WORKING OF SCREWS, BOLT HEADS, OR NUTS, IN CONJUNCTION THEREWITH
- B23G7/00—Forming thread by means of tools similar both in form and in manner of use to thread-cutting tools, but without removing any material
- B23G7/02—Tools for this purpose
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Drilling Tools (AREA)
Abstract
A tap tool T having passageways 14, 15 for the supply of fluid under high pressure and at a low flow rate is used to form threads in the wall of a preformed hole 12 in a component 10 formed of an aggressive material e.g. a metal matrix composite. The tap displaces the ductile phase of the metal matrix, and no material is cut away. <IMAGE>
Description
2 24 9510 1 COMPONENT WITH THREADED HOLE The invention relates to the
threading of a hole in a component made of a material in which it is difficult to form an internal thread in the wall of the hole by known methods. Such materials include so-called metal matrix composites, which consist of a continuous metal phase reinforced with a disperse phase which may or may not be metal. The continuous phase may be formed of a metal such as aluminium, magnesium, titanium or an alloy based on any of these; the disperse phase may be in particulate, fibre or whisker form and selected from a wide range of materials such as silicon carbide, boron carbide, alumina, carbon, sand and other refractory fillers; wires of steel, copper or silver; and the like. A typical metal matrix composite comprises from about 10% to 40% by volume of silicon carbide in a continuous phase of an alloy of aluminium/magnesium/silicon or aluminium/copper or aluminium/lithium. Composites are of value because of lightness in weight coupled with strength and stiffness properties which are exerted even at high temperatures. Such composites can be made by a wide variety of techniques. The component may be a part useful in the automotive or aerospace, aeronautical or construction industries. Other materials in which it is difficult to form threaded holes include so-called aggressive metals which present a resistance to being worked, e.g. ductile steels, titanium, and the like, and non-metallic compositions 2 such as particle boards, fibre based or reinforced materials.
It is one object of this invention to provide a method of making a threaded hole in a component made of a material in which it is otherwise difficult to form a threaded hole by known method. The invention is based on the discovery that a cold forming tool such as a tap can be used to form the threads. This appears to be possible because under the conditions of this invention the distribution of the disperse phase allows the tap to displace the more ductile continuous phase so allowing thread forming parts of the tool readily to form the required threads.
According to the invention in one aspect there is provided a method of threading the wall of a hole in a component composed of relatively ductile material, the method comprising urging a cold forming tool having thread-forming means into the hole characterised by supplying pressure resistant lubricant fluid, thereby to form the threaded wall.
Preferably, the cold forming tool has spaced apart thread forming rings and the pressure resistant lubricant fluid is directed to flow under pressure between adjacent rings into the gap between the tool and the wall to be threaded. The fluid may be introduced intermittently or continuously, as required. In a preferred feature, the tool has a main passage for the passage of the fluid, branch passages leading from the main passage to 3 outlets at the junction of adjacent rings. Many proposals exist in the literature to cut threads in metal see e.g. US-A-4693646 and DE-A-3307555 and DE-UM-A-G89 01178 and to provide a bore so that a lubricant and/or coolant liquid may flow therethrough.
These disclosures are not relevant to this invention where the tool operates by displacing metal and not cutting it, i.e. there is no swarf. Such thread cutting devices cannot be used with the ductile or aggressive materials of which the components relevant to this invention are formed. It is also proposed in US-A 2807813 to use a fluteless tap to form internal threads in a borehole in a ductile material but no liquid is present when that device is used. In contrast, in the present invention, a tap is used in association with the pressure-resistant liquid to form the desired threads in a particularly efficient and advantageous way.
The tool is preferably made of a high speed steel, e.g. cobalt steel, the use of which in the context is considered to be totally unexpected.
The lubricant fluid, which may be a liquid or gas, is preferably supplied at relatively high pressure (say 1200 psi) and a relatively low flow rate. The fluid is preferably also temperature resistant and is most preferably an extreme pressure resistant lubricant such as a gearbox oil.
4 The tool may be advanced into a preformed hole with rotation and/or by a rectilinear motion.
our investigations have established that where the continuous phase of a metal matrix composite is a ductile material, e.g. aluminium, the regions of component which are free of the disperse phase still have that ductility despite the presence of the dispersed hard or refractory particles in the matrix. When a thread forming tool of the invention is urged into the hole, the continuous phase being ductile yields under the insertion force, allowing the threads to be formed in the hole wall accurately and efficiently. The urging is done cold by rotating the tap or by rectilinear motion. No material is cut away, so there is no swarf etc. to be removed. There is some evidence to suggest that the wall portions defining the formed threads have a high concentration of the hard particles, which may provide increased strength and wear resistance.
The fluid is required because if fluid is not present the tool is subjected to severe wear and will usually last for a single use only. The volume of fluid required is very low, which implies that only a thin film of material is formed between the wall to be threaded and the thread former, which film must have lubricous and pressure resistant properties.
In other aspects, the invention includes a component having a hole therein, the wall of the hole being threaded, the threads having been formed in the wall of a preformed hole by the urging therein of a cold forming tool having thread-forming means; and a cold forming tool comprising a shank having spaced apart thread forming rings, means being provided to supply pressure resistant lubricant fluid to outlets adjacent and/or between the rings.
In order that the invention may be well understood it will now be described by way of example only with reference to the accompanying diagrammatic drawings, in which:
Figure 1 is a section of a component having a hole with generally smooth walls showing the thread forming tap, and Figure 2 is a section of the threaded hole.
The component C comprises a body 10 formed of a metal matrix composite such as a ductile aluminium/magnesium/silicon alloy containing hard particles of silicon carbide 11 dispersed therein. A hole 12 having straight side walls is formed, e.g. by punching, drilling or the like into the depth of the body 10. A cold forming tool T in the form of a tap has thread former rings 13 which are spaced apart longitudinal of the shank. A passage 14 extends through the shank and has branch passages 15 which open at the outlets 16 at the junction, i.e. roots of adjacent 6 rings 13. A lubricant which is pressure and temperature resistant, e.g. a gearbox oil, is passed through the outlets 16 at relatively high pressure but low flow rate to be interposed between the walls of the hole 12 and the tool T. The rings are dimensioned according to the size of threads to be formed. The tap T is then urged into the hole 12 using known equipment and then removed. The insertion cause the particles of the silicon carbide to be displaced away from the hole wall because of the ductility of the continuous phase of the metal matrix composite.
The hole has thereby been threaded at 20 by the rings 13 and the body retains its properties of lightness in weight, strength, stiffness and the like. It is surprising that a metal matrix composite can undergo deformation during the tapping leading to the formation of threads without any adverse effect. There is evidence that the particles are concentrated in the formed threads 20. The fluid appears to act lubriciously to allow the tool to move relative to the hole wall and to provide a boundary layer to reduce tool wear. The fluid may however play a more direct role in shaping the thread as there is evidence to suggest that the fluid on the tap contours presents a mould surface which deforms the wall of the hole.
The invention is not limited to the embodiment shown. The tool may be fluted to allow for escape of fluid; the fluid may be introduced in other ways; the fluid may be nitrogen; the component may be made of metal or a gas such as non-metal. The 7 hole may be blind or a through hole
Claims (25)
- A method of threading the wall of a hole (12) in a component (10) composed of relatively ductile material, the method comprising urging a cold forming tool (T) having threadforming means (13) into the hole (12) characterised by supplying pressure resistant lubricant fluid, thereby to form the threaded wall.
- 2. A method according to Claim 1, characterised in that the cold forming tool (T) has spaced apart thread forming rings (13) and the pressure resistant lubricant fluid is directed to flow under pressure between adjacent rings (13) into the gap between the tool (T) and the wall of the hole (12) to be threaded.
- 3.A method according to Claim 2, characterised in that the tool (T) has a main passage (14) for the passage of the fluid, branch passages (15) leading from the main passage to outlets (16) at the junction of adjacent rings (13).
- A method according to any preceding Claim, characterised in that the fluid is supplied at a relatively high pressure and a relatively low flow rate.
- C A method according to Claim 4, characterised in that the fluid is supplied under a pressure of about 1200 psi.
- A method according to any preceding Claim, characterised in that the fluid is also temperature resistant.
- 7.A method according to any preceding Claim, characterised in that the fluid is an extreme pressure resistant lubricant such as a gearbox oil.
- 8.A method according to any preceding Claim, characterised in that the cold forming tool (T) is advanced into the hole (12) with rotation.
- 9. A method according to any preceding Claim, that the tool is a thread forming tap.characterised in
- 10. A method according to Claim 9, characterised in that the tap is formed of a steel such as a high speed tool steel.
- 11. A method according to Claim 10, characterised in that the material of which the component is made is a metal matrix composite.
- 12. A method according to Claim 11, characterised in that the material comprises aluminium or the like as the continuous to phase of the matrix, and particles (11) of silicon carbon or like hard or refractory material are dispersed therein.
- 13. A method according to any of Claims 1 to 10, characterised in that the material of which the component is made comprises an aggressive metal, e.g. a steel.
- 14. A method according to any of Claims 1 to 10 characterised in that the material of which the component is made comprises a particle board.
- 15. A component (C) having a hole (12) therein, the wall of the hole (12) being threaded (20), the threads (20) having been formed in the wall of a preformed hole (12) by the urging therein of a cold forming tool (T) having thread-forming means (13) and means (14, 15) for the passage of a fluid therein under high pressure and a low flow rate.
- 16. A component according to Claim 15, characterised in that the component is made of a relatively ductile material.
- 17. A component according to Claim 15 or 16, characterised in that the component comprises a metal matrix composite.
- A component according comprising aluminium as the to Claim 17, characterised by continuous phase and particles (11) of silicon carbide or like refractory material as the disperse phase.
- 19. A component according to Claim 15 or 16, characterised in that the component is formed of particle board.
- 20. A cold forming tool (T) comprising a shank having spaced apart thread forming rings(13), characterised by means (14, 15) to supply pressure resistant lubricant fluid adjacent and/or between the rings.
- A tool according to Claim 20, characterised in that a main passage (14) for the fluid extends through the shank and branch passages (15) extend from the main passage to emerge at outlets (16) between adjacent rings.
- 22. A tool according to Claim 20 or 21 formed of a steel.characterised by being
- 23. A tool according to Claim 22, characterised by being formed of a cobalt steel.
- 24. A tool according to any of Claims 20 to 23, characterised in that passages in the thread forming rings have been shaped by spark erosion.1 \I-
- 25. A tool according to Claim 20 or 21, characterised in that the tool has been formed by powder metallurgy.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB909020223A GB9020223D0 (en) | 1990-09-14 | 1990-09-14 | Metal matrix composite component with threaded hole |
| GB919115662A GB9115662D0 (en) | 1991-07-19 | 1991-07-19 | Metal matrix composite component |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB9119619D0 GB9119619D0 (en) | 1991-10-23 |
| GB2249510A true GB2249510A (en) | 1992-05-13 |
| GB2249510B GB2249510B (en) | 1994-03-09 |
Family
ID=26297661
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9119619A Expired - Fee Related GB2249510B (en) | 1990-09-14 | 1991-09-13 | Component with threaded hole |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US5435786A (en) |
| EP (1) | EP0548195B1 (en) |
| JP (1) | JPH06500505A (en) |
| AU (1) | AU8506391A (en) |
| DE (1) | DE69110682D1 (en) |
| GB (1) | GB2249510B (en) |
| WO (1) | WO1992004997A1 (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SE512456C2 (en) * | 1997-04-11 | 2000-03-20 | Sandvik Ab | Tools for making internal threads |
| FR2985445B1 (en) * | 2012-01-05 | 2014-09-26 | Snecma | TOOL FOR THE MACHINING OF A WALL OF A WORKPIECE, IN PARTICULAR IN COMPOSITE MATERIAL. |
| US10773323B2 (en) * | 2018-08-21 | 2020-09-15 | Ford Motor Company | Minimum quantity lubrication thread tap |
| CN109352099B (en) * | 2018-12-07 | 2020-08-07 | 西安交通大学 | Screw tap with self-lubricating cooling structure |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2807813A (en) * | 1956-04-03 | 1957-10-01 | Besley Welles Corp | Fluteless swaging taps |
| US4539832A (en) * | 1983-09-19 | 1985-09-10 | Balax, Inc. | Hole sizing tool |
| US4693646A (en) * | 1986-02-18 | 1987-09-15 | Gemcor Engineering Corp. | Apparatus for lubricating a workpiece |
| US4762444A (en) * | 1987-03-16 | 1988-08-09 | Mena Carl M | Screw tap with lubrication and extraction bores |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1527200A1 (en) * | 1965-05-11 | 1971-07-01 | Vermont American Corp | Taps |
| DE3307555C2 (en) * | 1983-03-03 | 1985-07-11 | Gühring, Gottlieb, 7470 Albstadt | Hole post-processing tool |
| JPH01281819A (en) * | 1988-05-02 | 1989-11-13 | Nec Corp | Female screw formation method |
| JPH02100820A (en) * | 1988-06-20 | 1990-04-12 | Nachi Fujikoshi Corp | Rolled tap with oil hole |
| DE8901178U1 (en) * | 1989-02-03 | 1989-03-23 | Ringfeder Gmbh, 4150 Krefeld | Taps |
-
1991
- 1991-09-13 AU AU85063/91A patent/AU8506391A/en not_active Abandoned
- 1991-09-13 GB GB9119619A patent/GB2249510B/en not_active Expired - Fee Related
- 1991-09-13 WO PCT/GB1991/001576 patent/WO1992004997A1/en not_active Ceased
- 1991-09-13 DE DE69110682T patent/DE69110682D1/en not_active Expired - Lifetime
- 1991-09-13 EP EP91916493A patent/EP0548195B1/en not_active Expired - Lifetime
- 1991-09-13 JP JP3514991A patent/JPH06500505A/en active Pending
-
1993
- 1993-03-11 US US08/029,486 patent/US5435786A/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2807813A (en) * | 1956-04-03 | 1957-10-01 | Besley Welles Corp | Fluteless swaging taps |
| US4539832A (en) * | 1983-09-19 | 1985-09-10 | Balax, Inc. | Hole sizing tool |
| US4693646A (en) * | 1986-02-18 | 1987-09-15 | Gemcor Engineering Corp. | Apparatus for lubricating a workpiece |
| US4762444A (en) * | 1987-03-16 | 1988-08-09 | Mena Carl M | Screw tap with lubrication and extraction bores |
| WO1988006933A1 (en) * | 1987-03-16 | 1988-09-22 | Mena Carl M | Screw tap with lubrication and extraction bores |
Also Published As
| Publication number | Publication date |
|---|---|
| DE69110682D1 (en) | 1995-07-27 |
| GB9119619D0 (en) | 1991-10-23 |
| WO1992004997A1 (en) | 1992-04-02 |
| JPH06500505A (en) | 1994-01-20 |
| EP0548195A1 (en) | 1993-06-30 |
| EP0548195B1 (en) | 1995-06-21 |
| AU8506391A (en) | 1992-04-15 |
| US5435786A (en) | 1995-07-25 |
| GB2249510B (en) | 1994-03-09 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19950913 |